CN205602146U - Helicopter transmission device - Google Patents
Helicopter transmission device Download PDFInfo
- Publication number
- CN205602146U CN205602146U CN201620341292.XU CN201620341292U CN205602146U CN 205602146 U CN205602146 U CN 205602146U CN 201620341292 U CN201620341292 U CN 201620341292U CN 205602146 U CN205602146 U CN 205602146U
- Authority
- CN
- China
- Prior art keywords
- rotor
- tail
- photovoltaic panel
- casing
- photovoltaic board
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Landscapes
- Wind Motors (AREA)
Abstract
In order to overcome not enough that current helicopter transmission device exists, the utility model provides a helicopter transmission device, is the helicopter main part including the exterior casing that is equipped with the photovoltaic board, the casing photovoltaic board upper portion is equipped with controlling means, the casing it is equipped with little wind wheel motor to inlay between the controlling means of photovoltaic board and the tail -rotor, the casing the photovoltaic board, controlling means, the electrical property links to each other between little wind wheel motor, the casing little wind wheel motor quantity on the photovoltaic board is 3 just 3 little wind wheel motor are different models, the casing photovoltaic board end is equipped with the tail -rotor, the casing the surface of photovoltaic board is equipped with photovoltaic board and photovoltaic circuit. The beneficial effects of the utility model reside in that a plurality of little wind wheel motor that helicopter transmission device was equipped with can coordinate the combination and adjust the single tail -rotor of supplementary tradition, has improved the regulation precision of tail -rotor.
Description
Technical field
This utility model relates to a kind of helicopter accessory field devices, especially one and is provided with multiple mild wind turbin generator, can
The tail-rotor single to coordinate combination regulation auxiliary tradition, improves the helicopter actuating device of the regulation precision of tail-rotor.
Background technology
Helicopter is mainly set by body and lift (containing rotor and tail-rotor), power, transmission three digest journals and onboard flight
Standby grade forms.Rotor is typically passed through the machinery being made up of power transmission shaft and decelerator etc. by turboaxle motor or piston-mode motor
Drive system drives, it is possible to the counteracting force produced by blade tip jet drives.Scooter 300km/h during helicopter maximum
Above, the nearly 400km/h of underriding limit velocity, practical ceiling up to 6000 meters (world record is 12450m), general voyage up to
600～about 800km.Portable machine inside and outside auxiliary fuel tank ferry range is up to more than 2000km.Have according to the different helicopters that needs
Different take-off weights.What the heavy helicopter come into operation on our times was maximum is that Muscovite rice-26(maximum plays fly weight
Amount reaches 56t, payload 20t).Currently practical application is single-rotor helicopter and the twin-rotor helicopter of mechanically driver type,
Most with single-rotor helicopter quantity the most again.
At present, known helicopter actuating device structure is mainly to include gear mechanism housing and interior drive mechanism.This is straight
Rise machine actuating device function singleness and the regulation low problem of precision of tradition tail-rotor cannot be solved.
Summary of the invention
For the deficiency overcoming existing helicopter actuating device to exist, this utility model provides a kind of helicopter transmission
Device, this helicopter actuating device is provided with multiple mild wind turbin generator, can coordinate the tail-rotor that combination regulation auxiliary tradition is single,
Improve the regulation precision of tail-rotor.
This utility model solve the technical scheme is that this utility model of its technical problem include housing-photovoltaic panel,
Tail-rotor, control device, mild wind turbin generator.
This utility model main body includes housing-photovoltaic panel that appearance is provided with；Housing-photovoltaic panel top is provided with control device；
Inlay between control device and the tail-rotor of described housing-photovoltaic panel and be provided with mild wind turbin generator；Described housing-photovoltaic panel, control
Device processed, is electrical connected between mild wind turbin generator.
Mild wind turbin generator quantity in housing-photovoltaic panel is 3 and described individual mild wind turbin generator 4 is different model.
Housing-photovoltaic panel end is provided with tail-rotor.
The surface of described housing-photovoltaic panel is provided with photovoltaic panel and photovoltaic circuit.
The beneficial effects of the utility model are, are provided with multiple mild wind turbin generator, can coordinate combination regulation auxiliary tradition single
The tail-rotor of one, improves the regulation precision of tail-rotor.
Accompanying drawing explanation
With embodiment, this utility model is further illustrated below in conjunction with the accompanying drawings；
Fig. 1 is the structural map of helicopter drive arrangement embodiment；
Fig. 2 is the block diagram of helicopter drive arrangement embodiment.
In figure
1, housing-photovoltaic panel
2, tail-rotor
3, device is controlled
4, mild wind turbin generator.
Detailed description of the invention
In embodiment as shown in Figure 1-2, this utility model includes housing-photovoltaic panel 1, tail-rotor 2, controls device 3, mild wind
Turbin generator 4.
This utility model main body includes that housing-photovoltaic panel 1 that appearance is provided with, housing-photovoltaic panel 1 end are provided with tail-rotor 2.Institute
The surface of the housing-photovoltaic panel 1 stated is provided with photovoltaic panel and photovoltaic circuit.Housing-photovoltaic panel 1 top is provided with control device 3；Described
Housing-photovoltaic panel 1 control device 3 and tail-rotor 2 between inlay and be provided with mild wind turbin generator 4；Mild wind in housing-photovoltaic panel 1
Turbin generator 4 quantity is 3 and described 3 mild wind turbin generators 4 are different models.Described housing-photovoltaic panel 1, controls dress
Put 3, be electrical connected between mild wind turbin generator 4.
When being embodied as, this utility model is provided with multiple mild wind turbin generator 4, can coordinate combination regulation auxiliary tradition single
The tail-rotor of one, improves the regulation precision of tail-rotor.
As known by the technical knowledge, this utility model can be by other essence without departing from its spirit or the reality of essential feature
The scheme of executing realizes.Embodiment disclosed above, for each side, is all merely illustrative, and is not only.All
All it is included in the utility model in the range of this utility model or being equal to the change in the range of this utility model.
Claims (1)
1. a helicopter actuating device, including housing-photovoltaic panel, tail-rotor, control device, mild wind turbin generator, is characterized in that: straight
Rise owner's body and include housing-photovoltaic panel that appearance is provided with；Housing-photovoltaic panel top is provided with control device；Described housing-photovoltaic
Inlay between control device and the tail-rotor of plate and be provided with mild wind turbin generator；Described housing-photovoltaic panel, controls device, mild wind wheel electricity
It is electrical connected between machine；Mild wind turbin generator quantity in housing-photovoltaic panel is 3 and described 3 mild wind turbin generators are different
Model；Housing-photovoltaic panel end is provided with tail-rotor；The surface of housing-photovoltaic panel is provided with photovoltaic panel and photovoltaic circuit.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620341292.XU CN205602146U (en) | 2016-04-21 | 2016-04-21 | Helicopter transmission device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620341292.XU CN205602146U (en) | 2016-04-21 | 2016-04-21 | Helicopter transmission device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205602146U true CN205602146U (en) | 2016-09-28 |
Family
ID=56970029
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620341292.XU Expired - Fee Related CN205602146U (en) | 2016-04-21 | 2016-04-21 | Helicopter transmission device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205602146U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108750102A (en) * | 2018-05-25 | 2018-11-06 | 清华大学 | A kind of electronic tail-rotor driving device of helicopter |
-
2016
- 2016-04-21 CN CN201620341292.XU patent/CN205602146U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108750102A (en) * | 2018-05-25 | 2018-11-06 | 清华大学 | A kind of electronic tail-rotor driving device of helicopter |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN102897316B (en) | Convertiplane and method of operation thereof | |
| CN204606221U (en) | A kind of many rotor fuel-electrics energy conversion aircraft | |
| CN201678037U (en) | Natural power levitation platform | |
| CN205239886U (en) | Aerostatics | |
| CN204660023U (en) | Aircraft | |
| CN206520748U (en) | A kind of oil electric mixed dynamic multi-rotor unmanned aerial vehicle | |
| CN104670504B (en) | Oil/optical electrical multi power source Fixed Wing AirVehicle | |
| CN105173092A (en) | Hybrid power multi-shaft rotor wing unmanned aerial vehicle | |
| CN208963310U (en) | It is a kind of can VTOL vert the fixed-wing unmanned plane of quadrotor | |
| CN103879555B (en) | A kind of driven type helicopter tail rotor drive system | |
| CN106477053A (en) | A kind of oil electricity mixes many rotor unmanned aircrafts | |
| CN104590535A (en) | Propelling device for airship power device | |
| CN205293073U (en) | Oil moves and directly drives many rotor crafts | |
| CN104986328A (en) | Variable-propeller-pitch multi-rotor aircraft driven by multiple oil engines | |
| CN204173160U (en) | The combustion engine powered multirotor helicopter of modularization | |
| CN205602146U (en) | Helicopter transmission device | |
| CN206288230U (en) | Full electricity autogyro | |
| CN207466966U (en) | A kind of dynamic displacement quadrotor unmanned plane of oil | |
| CN106114097A (en) | One can vertical take-off and landing flying car | |
| CN204489180U (en) | The two duct aircraft of a kind of coaxial rotor | |
| CN105905293B (en) | A kind of oil electricity mixing multi-rotor aerocraft | |
| CN205602123U (en) | Helicopter tail -rotor | |
| CN209506082U (en) | Dual rotation propeller oil electricity mixing fire-fighting unmanned plane | |
| CN206704550U (en) | To the depopulated helicopter fuselage interior structure of arrangement after a kind of turboaxle motor | |
| CN202481307U (en) | Four-propeller aircraft taking off and landing vertically |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160928 Termination date: 20170421 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |